| 摘要 |
The method involves applying individual non-servo-controlled control to motors so as to cause a rotary-wing drone to rotate about a rotation axis from an initial angular position to a predetermined intermediate angular position. The individual control is applied to the motors servo-controlled to a reference target trajectory (10) so as to finish off the rotation of the drone through one complete turn about the rotation axis progressively from the intermediate angular position with a non-zero angular velocity to a final angular position with a zero angular velocity. An independent claim is also included for a software comprising set of instructions for executing a method for dynamically controlling attitude of a rotary-wing drone to automatically execute a roll or loop-type preprogrammed-type maneuver. |
